US6390476B1 - Heat-resistant magnetic silicone rubber brush seals in turbomachinery and methods of application - Google Patents

Heat-resistant magnetic silicone rubber brush seals in turbomachinery and methods of application Download PDF

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Publication number
US6390476B1
US6390476B1 US09/657,527 US65752700A US6390476B1 US 6390476 B1 US6390476 B1 US 6390476B1 US 65752700 A US65752700 A US 65752700A US 6390476 B1 US6390476 B1 US 6390476B1
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Prior art keywords
component
brush seal
seal body
groove
brush
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US09/657,527
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Wei Tong
Zhangqing Zhuo
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General Electric Co
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General Electric Co
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Priority to US09/657,527 priority Critical patent/US6390476B1/en
Application filed by General Electric Co filed Critical General Electric Co
Assigned to GENERAL ELECTRIC COMPANY reassignment GENERAL ELECTRIC COMPANY ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: TONG, WEI, ZHUO, ZHANGQING
Assigned to ENERGY, UNITED STATES, DEPARTMENT OF reassignment ENERGY, UNITED STATES, DEPARTMENT OF CONFIRMATORY LICENSE (SEE DOCUMENT FOR DETAILS). Assignors: GENERAL ELECTRIC COMPANY
Priority to EP01964067A priority patent/EP1234130B1/en
Priority to JP2002525404A priority patent/JP2004508520A/en
Priority to DE60106861T priority patent/DE60106861T2/en
Priority to PCT/US2001/025617 priority patent/WO2002021027A1/en
Priority to AT01964067T priority patent/ATE281618T1/en
Publication of US6390476B1 publication Critical patent/US6390476B1/en
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    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16J—PISTONS; CYLINDERS; SEALINGS
    • F16J15/00—Sealings
    • F16J15/16—Sealings between relatively-moving surfaces
    • F16J15/32—Sealings between relatively-moving surfaces with elastic sealings, e.g. O-rings
    • F16J15/3284—Sealings between relatively-moving surfaces with elastic sealings, e.g. O-rings characterised by their structure; Selection of materials
    • F16J15/3288—Filamentary structures, e.g. brush seals
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16J—PISTONS; CYLINDERS; SEALINGS
    • F16J15/00—Sealings
    • F16J15/44—Free-space packings
    • F16J15/441—Free-space packings with floating ring
    • F16J15/442—Free-space packings with floating ring segmented

Definitions

  • the present invention relates to brush seals for use in turbomachinery such as gas and steam turbines to minimize leakage flows and particularly to a flexible heat-resistant magnetic silicone rubber brush seal useful over a wide range of sealing dimensions.
  • the present invention further relates to a flexible brush seal formed of a magnetic material for at least temporarily adhering the brush seal to one of the sealing components to facilitate installation, either as original equipment or as a retrofit.
  • seals are used at different locations for minimizing leakage flows.
  • seals may be provided between sealing surfaces which are both movable relative to one another or between components in which one component moves relative to another component, e.g., a stationary housing and a rotating shaft.
  • Brush seals typically comprise a plurality of elongated wire bristles in contact with a movable, e.g., rotating surface.
  • the bristles provide a tight rub-tolerant seal which experiences only slight degradation over time.
  • the bristles of the seal are compliant in use and this minimizes damage due to transient impact between the sealing components.
  • a typical brush seal is formed by folding bristles over a rod with an outer clamp maintaining the folded bristles, squeezing the bristles between a folded metal plate forming a clamp or sandwiching the bristles between a pair of supporting metal plates and welding the plates and bristles at their proximal ends to one another.
  • the distal ends of the bristles typically project a certain distance from the margins of the backing plates or clamps to engage the opposing sealing component.
  • the bristle holder or carrier is formed of metal which is usually machined with a tight tolerance and thus the brush seal is applicable to only a specific sealing dimension.
  • a separately manufactured and distinct brush seal must be used in order to dimensionally fit the seal with its carrier. Consequently, the brush seals are costly in terms of tooling, manufacturing and installation and long cycle times in brush seal manufacturing and retrofitting are required. Accordingly, there is a need for an improved brush seal where one size fits many different sizes of brush seals. Additionally, there is a need to facilitate installation of a brush seal without use of ancillary jigs or fixtures typically necessary to hold or temporarily secure the brush seal to its carrier.
  • a brush seal having a seal body formed of a flexible magnetic material such as a heat-resistant magnetic silicone rubber material.
  • the bristles are embedded, glued or otherwise secured to the brush seal body such that the bristles project from the body, terminating in tips for sealing engagement with the opposing sealing component.
  • the brush seal can fit a wide range of sealing dimensions and complex sealing geometry. For example, where the brush seal is to be applied between a fixed annulus and a shaft rotating within the annulus, the brush seal body may be flexed to conform to the dimensions of the two components.
  • the brush body can be used for either outer sealing where the bristles point radially outward, inner sealing where the bristles point radially inward, or axial sealing where the bristles point parallel to the rotor axis.
  • This type of brush seal is particularly suitable for large sealing dimensions, such as forty inches or more.
  • the brush seal body can be flexed or bent into virtually any irregular shape, for example, a non-linear shape other than circular, and thus may be used for sealing between irregularly-shaped components.
  • An example of the latter is a brush seal interposed between a transition piece and a first-stage nozzle in a gas turbine.
  • the seal may be readily adhered to one of the sealing components.
  • the adherence is temporary until the seal body can be finally adjusted and secured in its desired position.
  • Ancillary jigs or fixtures useful to maintain the brush seal body in position while adjustments are being made prior to final securement are entirely eliminated.
  • a magnetic silicone rubber is preferred and comprises a composite material of ferrite magnetic powder and a silicone polymer. With those characteristics, the brush seal body can be bent, twisted or coiled and thus easily configured for installation.
  • a brush seal for sealing between first and second components movable relative to one another and having non-linear opposed sealing surfaces, comprising a brush seal body carried by the first component and having a plurality of bristles secured to the body and projecting therefrom to terminate in bristle tips for engaging the second component, the brush seal body being formed of a flexible material for conformance to the non-linear opposed sealing surfaces.
  • a brush seal for sealing between first and second components movable relative to one another and having non-linear opposed sealing surfaces, comprising a brush seal body carried by the first component and having a plurality of bristles secured to the body and projecting therefrom to terminate in bristle tips for engaging the second component, the brush seal body being formed of a magnetic material for magnetic attachment to the non-linear opposed sealing surface of one component.
  • a method of forming a brush seal between first and second components movable relative to one another comprising the steps of providing a brush seal body formed of magnetic material and having a plurality of bristles projecting therefrom terminating in tips for engagement with the second component and magnetically adhering the brush seal body to the first component.
  • a method of forming a brush seal between first and second components movable relative to one another comprising the steps of providing a brush seal body formed of a flexible material and having a plurality of bristles projecting therefrom terminating in tips for engagement with the second component and flexing the brush seal body for conformance to the first component.
  • FIG. 1 is a fragmentary cross-sectional view illustrating a brush seal constructed in accordance with a preferred embodiment of the present invention installed in a high pressure packing;
  • FIG. 2 is a view similar to FIG. 1 illustrating the brush seal hereof similarly as shown in FIG. 1 in a bearing;
  • FIG. 3 is a perspective view of the brush seal in linear form prior to bending or flexing for use in a seal.
  • Brush seal 10 includes a brush seal body 12 and a plurality of bristles 14 forming a bristle pack 16 carried by the brush seal body 12 .
  • the brush seal body 12 is comprised of a heat-resistant magnetic flexible silicone rubber material in the general shape of an elongated channel having a base 18 and opposite sides 20 and 22 .
  • the bristle pack 16 comprises a plurality of bristles 14 disposed in the groove or channel 24 of the body 12 terminating in bristle tips 17 .
  • the bristles are elongated, formed of metal and have diameters ranging from 0.002 to 0.01 inch, depending upon the temperature, pressure and sealing pattern in which the bristles are to be used. It will be appreciated that non-metal materials such as aramid fibers, e.g., KEVLAR®, may be utilized, particularly in view of their capacity to operate at high temperature conditions, for example, up to 425° C.
  • the rubber material selected for the brush seal body 12 has substantial resistance to high temperatures. Silicone rubbers, for example, have high temperature resistance, up to 325° C., and also remain flexible at very low temperatures.
  • a magnetic silicone rubber comprised of a ferrite magnetic powder and silicone polymer is used.
  • the brush seal body 12 and bristles 14 can be bent, twisted, coiled and easily fabricated.
  • the body 12 need not be formed of one piece.
  • the flexible material may comprise a pair of backing pieces joined to one another at the base 18 and to the bristles. Alternatively, the proximal ends of the bristles may be secured in or to a base piece, in turn secured to a pair of side pieces.
  • the seal 10 has many applications.
  • the seal 10 is employed in a high pressure packing in a turbine.
  • An inner barrel 30 comprising a first stationary component is generally concentrically arranged about an aft stub shaft 32 comprising a second rotating component.
  • a brush seal 10 is mounted adjacent the end of the barrel in annular sealing relation about the stub shaft 32 , the bristle tips 17 lying in engagement with the surface of the shaft 32 .
  • the labyrinth-type seals 34 disposed annularly about the grooves 35 of the stub shaft 32 for forming a labyrinth seal in combination with the brush seal 10 .
  • the brush seal 10 is mounted in a groove 36 formed on the end of the barrel.
  • the brush seal 10 is secured to the barrel 30 in the groove 36 by an overlying annular or arcuately segmented end plate 38 secured to the barrel 30 , for example, by bolts 40 .
  • the end plate 38 has a lower tapered annular edge 42 for retaining the brush seal 10 in the groove 36 .
  • the brush seal 10 is formed in a linear extending strip.
  • the silicone rubber material may be extruded in the form of a channel with the bristles planted in the base of the channel-shaped extrusion, the bristles extending at a cant angle relative to the longitudinal dimension of the linear brush seal strip.
  • the bristles may be glued between the two sides and to the base of the strip.
  • the bristles are typically inclined relative to the longitudinal length of the strip at a cant angle of about 40 to 50° relative to a plane passing perpendicularly through the strip.
  • the strip may be installed in discrete arcuate segments or as a unitary strip extending completely between the two components being sealed.
  • the brush seal 10 can be flexed into an annular form or into arcuate segments to conform to the arcuate dimensions of the groove 36 .
  • the strip can be cut to the appropriate length and flexed for reception in the groove 36 .
  • the magnetic material of the brush seal 10 provides a magnetic attraction with the metal of the barrel 30 . Consequently, the brush seal can be disposed in the groove 36 and temporarily held in the groove by magnetic attraction while the end plate 38 is applied to finally secure the brush seal in the groove. It will be appreciated that the brush seal may be flexed to a wide range of different diameters or radii where arcuate segments are being used as well as into irregular shapes for other seal applications.
  • FIG. 2 Another application of the brush seal 10 hereof is illustrated in FIG. 2 .
  • a seal carrier 50 forming part of a bearing is illustrated with the brush seal 10 installed in a groove 52 of the carrier 50 .
  • the brush seal 10 is cut to length for conformance to the arcuate dimensions of the groove 52 .
  • the brush seal can then be flexed for location in the groove 52 with the magnetic material temporarily maintaining the brush seal in the groove.
  • the annular or segmented end plate 54 is then secured to the seal carrier 50 to finally secure the brush seal in the groove.
  • the brush seal as illustrated, is used in conjunction with labyrinth teeth 55 formed on the seal carrier 50 .
  • a rubber brush seal can be used for outer sealing where the bristles point radially outwardly, inner sealing where the bristles point radially inwardly as in the seals illustrated in FIGS. 1 and 2, or axial seals where the bristles point parallel to the rotor axis.
  • the sealing strip can be flexed or bent both in the plane of the bristles to form an annular seal such as illustrated in FIGS. 1 and 2, or about an axis normal thereto to provide an axial projecting brush seal.
  • the leakage control is provided by both the brush seal and the labyrinth seal teeth.
  • the flexible nature of the brush seal enables the brush seal to be used in most sealing applications in turbomachinery and particularly without regard to the dimensions of the sealing surfaces. That is, the brush seal can be flexed to accommodate various arcuate or irregular dimensions and cut to length, thereby providing a seal where one size, for example, as illustrated in FIG. 3, fits a substantial number of different seal applications and dimensions in the turbomachinery.

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Sealing Devices (AREA)
  • Manufacture Of Motors, Generators (AREA)
  • Laminated Bodies (AREA)

Abstract

A brush seal includes a brush seal body formed of heat-resistant magnetic silicone rubber material in the form of a channel. Bristles are disposed in the channel of the brush seal body at a cant angle and project from the edges of the body terminating in bristle tips. The brush seal is formed linearly and, in use, flexed to form an annular seal between adjacent annular sealing components, with the seal carried by one component and the bristle tips engaging the opposite component. The magnetic material of the seal body enables temporary securement of the seal to one of the components, while the seal is adjusted and finally secured in place.

Description

BACKGROUND OF THE INVENTION
The present invention relates to brush seals for use in turbomachinery such as gas and steam turbines to minimize leakage flows and particularly to a flexible heat-resistant magnetic silicone rubber brush seal useful over a wide range of sealing dimensions. The present invention further relates to a flexible brush seal formed of a magnetic material for at least temporarily adhering the brush seal to one of the sealing components to facilitate installation, either as original equipment or as a retrofit.
In turbomachinery such as gas and steam turbines, compressors and turbopumps, a number of seals are used at different locations for minimizing leakage flows. For example, seals may be provided between sealing surfaces which are both movable relative to one another or between components in which one component moves relative to another component, e.g., a stationary housing and a rotating shaft.
Brush seals, particularly in turbomachinery, typically comprise a plurality of elongated wire bristles in contact with a movable, e.g., rotating surface. The bristles provide a tight rub-tolerant seal which experiences only slight degradation over time. The bristles of the seal are compliant in use and this minimizes damage due to transient impact between the sealing components. A typical brush seal is formed by folding bristles over a rod with an outer clamp maintaining the folded bristles, squeezing the bristles between a folded metal plate forming a clamp or sandwiching the bristles between a pair of supporting metal plates and welding the plates and bristles at their proximal ends to one another. The distal ends of the bristles typically project a certain distance from the margins of the backing plates or clamps to engage the opposing sealing component. Common to these types of brush seals is that the bristle holder or carrier is formed of metal which is usually machined with a tight tolerance and thus the brush seal is applicable to only a specific sealing dimension. For other sealing dimensions, e.g., diameters, a separately manufactured and distinct brush seal must be used in order to dimensionally fit the seal with its carrier. Consequently, the brush seals are costly in terms of tooling, manufacturing and installation and long cycle times in brush seal manufacturing and retrofitting are required. Accordingly, there is a need for an improved brush seal where one size fits many different sizes of brush seals. Additionally, there is a need to facilitate installation of a brush seal without use of ancillary jigs or fixtures typically necessary to hold or temporarily secure the brush seal to its carrier.
BRIEF SUMMARY OF THE INVENTION
In accordance with a preferred embodiment of the present invention, there is provided a brush seal having a seal body formed of a flexible magnetic material such as a heat-resistant magnetic silicone rubber material. Preferably, the bristles are embedded, glued or otherwise secured to the brush seal body such that the bristles project from the body, terminating in tips for sealing engagement with the opposing sealing component. It will be appreciated that by bending the magnetic silicone rubber of the brush seal body, the brush seal can fit a wide range of sealing dimensions and complex sealing geometry. For example, where the brush seal is to be applied between a fixed annulus and a shaft rotating within the annulus, the brush seal body may be flexed to conform to the dimensions of the two components. Additionally, by changing the brush bending pattern, the brush body can be used for either outer sealing where the bristles point radially outward, inner sealing where the bristles point radially inward, or axial sealing where the bristles point parallel to the rotor axis. This type of brush seal is particularly suitable for large sealing dimensions, such as forty inches or more. It will also be appreciated that the brush seal body can be flexed or bent into virtually any irregular shape, for example, a non-linear shape other than circular, and thus may be used for sealing between irregularly-shaped components. An example of the latter is a brush seal interposed between a transition piece and a first-stage nozzle in a gas turbine.
Additionally, by forming the brush seal body from a magnetic silicone rubber, the seal may be readily adhered to one of the sealing components. Preferably, the adherence is temporary until the seal body can be finally adjusted and secured in its desired position. Ancillary jigs or fixtures useful to maintain the brush seal body in position while adjustments are being made prior to final securement are entirely eliminated. A magnetic silicone rubber is preferred and comprises a composite material of ferrite magnetic powder and a silicone polymer. With those characteristics, the brush seal body can be bent, twisted or coiled and thus easily configured for installation.
In a preferred embodiment according to the present invention, there is provided a brush seal for sealing between first and second components movable relative to one another and having non-linear opposed sealing surfaces, comprising a brush seal body carried by the first component and having a plurality of bristles secured to the body and projecting therefrom to terminate in bristle tips for engaging the second component, the brush seal body being formed of a flexible material for conformance to the non-linear opposed sealing surfaces.
In a further preferred embodiment according to the present invention, there is provided a brush seal for sealing between first and second components movable relative to one another and having non-linear opposed sealing surfaces, comprising a brush seal body carried by the first component and having a plurality of bristles secured to the body and projecting therefrom to terminate in bristle tips for engaging the second component, the brush seal body being formed of a magnetic material for magnetic attachment to the non-linear opposed sealing surface of one component.
In a still further preferred embodiment according to the present invention, there is provided a method of forming a brush seal between first and second components movable relative to one another, comprising the steps of providing a brush seal body formed of magnetic material and having a plurality of bristles projecting therefrom terminating in tips for engagement with the second component and magnetically adhering the brush seal body to the first component.
In a still further preferred embodiment according to the present invention, there is provided a method of forming a brush seal between first and second components movable relative to one another, comprising the steps of providing a brush seal body formed of a flexible material and having a plurality of bristles projecting therefrom terminating in tips for engagement with the second component and flexing the brush seal body for conformance to the first component.
BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1 is a fragmentary cross-sectional view illustrating a brush seal constructed in accordance with a preferred embodiment of the present invention installed in a high pressure packing;
FIG. 2 is a view similar to FIG. 1 illustrating the brush seal hereof similarly as shown in FIG. 1 in a bearing; and
FIG. 3 is a perspective view of the brush seal in linear form prior to bending or flexing for use in a seal.
DETAILED DESCRIPTION OF THE INVENTION
Referring now to the drawings, there is illustrated a brush seal, generally designated 10, constructed in accordance with a preferred embodiment of the present invention. Brush seal 10 includes a brush seal body 12 and a plurality of bristles 14 forming a bristle pack 16 carried by the brush seal body 12. In a preferred embodiment, the brush seal body 12 is comprised of a heat-resistant magnetic flexible silicone rubber material in the general shape of an elongated channel having a base 18 and opposite sides 20 and 22. The bristle pack 16 comprises a plurality of bristles 14 disposed in the groove or channel 24 of the body 12 terminating in bristle tips 17. Typically, the bristles are elongated, formed of metal and have diameters ranging from 0.002 to 0.01 inch, depending upon the temperature, pressure and sealing pattern in which the bristles are to be used. It will be appreciated that non-metal materials such as aramid fibers, e.g., KEVLAR®, may be utilized, particularly in view of their capacity to operate at high temperature conditions, for example, up to 425° C.
Because turbomachinery typically operates at high temperature, the rubber material selected for the brush seal body 12 has substantial resistance to high temperatures. Silicone rubbers, for example, have high temperature resistance, up to 325° C., and also remain flexible at very low temperatures. Preferably, a magnetic silicone rubber comprised of a ferrite magnetic powder and silicone polymer is used. With those characteristics, the brush seal body 12 and bristles 14 can be bent, twisted, coiled and easily fabricated. It will also be appreciated that the body 12 need not be formed of one piece. For example, the flexible material may comprise a pair of backing pieces joined to one another at the base 18 and to the bristles. Alternatively, the proximal ends of the bristles may be secured in or to a base piece, in turn secured to a pair of side pieces.
The seal 10 has many applications. For example, in FIG. 1, the seal 10 is employed in a high pressure packing in a turbine. An inner barrel 30 comprising a first stationary component is generally concentrically arranged about an aft stub shaft 32 comprising a second rotating component. A brush seal 10 is mounted adjacent the end of the barrel in annular sealing relation about the stub shaft 32, the bristle tips 17 lying in engagement with the surface of the shaft 32. Note the labyrinth-type seals 34 disposed annularly about the grooves 35 of the stub shaft 32 for forming a labyrinth seal in combination with the brush seal 10. Preferably, the brush seal 10 is mounted in a groove 36 formed on the end of the barrel. The brush seal 10 is secured to the barrel 30 in the groove 36 by an overlying annular or arcuately segmented end plate 38 secured to the barrel 30, for example, by bolts 40. The end plate 38 has a lower tapered annular edge 42 for retaining the brush seal 10 in the groove 36.
It will be appreciated that the brush seal 10 is formed in a linear extending strip. For example, the silicone rubber material may be extruded in the form of a channel with the bristles planted in the base of the channel-shaped extrusion, the bristles extending at a cant angle relative to the longitudinal dimension of the linear brush seal strip. Where a pair of discrete sides are secured to one another to form the brush seal strip, the bristles may be glued between the two sides and to the base of the strip. The bristles are typically inclined relative to the longitudinal length of the strip at a cant angle of about 40 to 50° relative to a plane passing perpendicularly through the strip. Also, the strip may be installed in discrete arcuate segments or as a unitary strip extending completely between the two components being sealed.
To install the strip onto the inner barrel 30 of FIG. 1, the brush seal 10 can be flexed into an annular form or into arcuate segments to conform to the arcuate dimensions of the groove 36. Once the long dimension of the brush seal strip is determined, the strip can be cut to the appropriate length and flexed for reception in the groove 36. The magnetic material of the brush seal 10 provides a magnetic attraction with the metal of the barrel 30. Consequently, the brush seal can be disposed in the groove 36 and temporarily held in the groove by magnetic attraction while the end plate 38 is applied to finally secure the brush seal in the groove. It will be appreciated that the brush seal may be flexed to a wide range of different diameters or radii where arcuate segments are being used as well as into irregular shapes for other seal applications.
Another application of the brush seal 10 hereof is illustrated in FIG. 2. In FIG. 2, a seal carrier 50 forming part of a bearing is illustrated with the brush seal 10 installed in a groove 52 of the carrier 50. As in the prior embodiment, the brush seal 10 is cut to length for conformance to the arcuate dimensions of the groove 52. The brush seal can then be flexed for location in the groove 52 with the magnetic material temporarily maintaining the brush seal in the groove. The annular or segmented end plate 54 is then secured to the seal carrier 50 to finally secure the brush seal in the groove. The brush seal, as illustrated, is used in conjunction with labyrinth teeth 55 formed on the seal carrier 50.
As noted previously, by changing the brush bending pattern, a rubber brush seal can be used for outer sealing where the bristles point radially outwardly, inner sealing where the bristles point radially inwardly as in the seals illustrated in FIGS. 1 and 2, or axial seals where the bristles point parallel to the rotor axis. Thus, it will be appreciated that the sealing strip can be flexed or bent both in the plane of the bristles to form an annular seal such as illustrated in FIGS. 1 and 2, or about an axis normal thereto to provide an axial projecting brush seal. In each of the illustrated embodiments of FIGS. 1 and 2, the leakage control is provided by both the brush seal and the labyrinth seal teeth.
It will be appreciated from the foregoing description of the brush seal hereof that the flexible nature of the brush seal enables the brush seal to be used in most sealing applications in turbomachinery and particularly without regard to the dimensions of the sealing surfaces. That is, the brush seal can be flexed to accommodate various arcuate or irregular dimensions and cut to length, thereby providing a seal where one size, for example, as illustrated in FIG. 3, fits a substantial number of different seal applications and dimensions in the turbomachinery.
While the invention has been described in connection with what is presently considered to be the most practical and preferred embodiment, it is to be understood that the invention is not to be limited to the disclosed embodiment, but on the contrary, is intended to cover various modifications and equivalent arrangements included within the spirit and scope of the appended claims.

Claims (22)

What is claimed is:
1. A brush seal for sealing between first and second components movable relative to one another and having non-linear opposed sealing surfaces, comprising:
a brush seal body carried by said first component and having a plurality of bristles secured to said body and projecting therefrom to terminate in bristle tips for engaging said second component;
said brush seal body being formed of a flexible magnetic material for conformance to the non-linear opposed sealing surfaces.
2. A brush seal according to claim 1 in combination with said first and second components, said first component including a groove for receiving said brush seal body.
3. A combination according to claim 2, wherein said groove opens through an end face of said first component, a brush seal holder overlying said end face and said brush seal body for retaining said brush seal body in said groove, and a fastener connecting said holder and said first component to one another.
4. A combination according to claim 3, wherein said first component includes a plurality of labyrinth seal teeth extending therefrom toward said second component.
5. A combination according to claim 4, wherein said first component comprises a stationary annular component and said second component comprises a rotatable shaft surrounded by said first component and engaged by said bristle tips.
6. A brush seal for sealing between first and second components movable relative to one another and having non-linear opposed sealing surfaces, comprising:
a brush seal body carried by said first component and having a plurality of bristles secured to said body and projecting therefrom to terminate in bristle tips for engaging said second component;
said brush seal body being formed of a flexible material for conformance to the non-linear opposed sealing surfaces;
said material comprising a silicone rubber material.
7. A brush seal according to claim 6, wherein said body has a length and is generally channel-shaped in cross-section, said bristles at least partially disposed within the channel of said channel-shaped cross-section of said body.
8. A brush seal for sealing between first and second components movable relative to one another and having non-linear opposed sealing surfaces, comprising:
a brush seal body carried by said first component and having a plurality of bristles secured to said body and projecting therefrom to terminate in bristle tips for engaging said second component;
said brush seal body being formed of a magnetic material for magnetic attachment to the non-linear opposed sealing surface of said one component.
9. A brush seal according to claim 8, wherein said material comprises a flexible silicone rubber material enabling the body for conformance to the sealing surface of said one component.
10. A brush seal according to claim 9, wherein said body has a length and is generally channel-shaped in cross-section, said bristles at least partially disposed within the channel of said channel-shaped cross-section of said body.
11. A brush seal according to claim 8, in combination with said first and second components, said first component including a groove for receiving said brush seal body.
12. A brush seal according to claim 11, wherein said groove opens through an end face of said first component and a brush seal holder overlying said end face and said brush seal body for retaining said brush seal body in said groove, and a fastener connecting said holder and said first component to one another.
13. A brush seal according to claim 12 wherein said first component includes a plurality of labyrinth seal teeth extending therefrom toward said second component.
14. A brush seal according to claim 13 wherein said first component comprises a stationary annular component and said second component comprises a rotatable shaft surrounded by said first component and engaged by said bristle tips.
15. A method of forming a brush seal between first and second components movable relative to one another, comprising the steps of:
providing a brush seal body formed of magnetic material and having a plurality of bristles projecting therefrom terminating in tips for engagement with the second component; and
magnetically adhering the brush seal body to the first component.
16. A method according to claim 15 including temporarily magnetically adhering the brush seal body to the first component and thereafter finally securing the brush seal body to the first component to form a seal with the second component.
17. A method according to claim 15 including providing a brush seal body of flexible material and flexing the body to conform to a mounting surface on said first component for mounting the seal body on said first component.
18. A method according to claim 17, wherein said first component comprises a stationary annular component and said second component comprises a rotatable shaft surrounded by said first component, forming a groove in said stationary fixed component for receiving said body, temporarily magnetically adhering the brush seal body in said groove and thereafter finally securing the brush seal body to the first component to form a seal with the second component.
19. A method of forming a brush seal between first and second components movable relative to one another, comprising the steps of:
providing a brush seal body formed of a flexible magnetic material and having a plurality of bristles projecting therefrom terminating in tips for engagement with the second component; and
flexing the brush seal body for conformance to the first component.
20. A method according to claim 19 wherein said first component comprises a stationary annular component and said second component comprises a rotatable shaft surrounded by said first component, forming a groove in said stationary fixed component for receiving said body, flexing the brush seal body for disposition in said groove and thereafter finally securing the brush seal body to the first component to form a seal with the second component.
21. A method according to claim 19 including magnetically adhering the brush seal body to one of said components.
22. A method according to claim 19 wherein the first component comprises a stationary annular component and the second component comprises a rotatable shaft surrounding said first component and including forming a groove in said stationary component and magnetically adhering said body in said groove.
US09/657,527 2000-09-08 2000-09-08 Heat-resistant magnetic silicone rubber brush seals in turbomachinery and methods of application Expired - Fee Related US6390476B1 (en)

Priority Applications (6)

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US09/657,527 US6390476B1 (en) 2000-09-08 2000-09-08 Heat-resistant magnetic silicone rubber brush seals in turbomachinery and methods of application
EP01964067A EP1234130B1 (en) 2000-09-08 2001-08-16 Heat-resistant magnetic silicone rubber body for brush seals in turbomachinery and methods of application
AT01964067T ATE281618T1 (en) 2000-09-08 2001-08-16 HEAT-RESISTANT BASE BODY MADE OF MAGNETIC SILICONE RUBBER FOR A BRUSH SEAL IN TURBO MACHINES AND METHOD FOR USE
JP2002525404A JP2004508520A (en) 2000-09-08 2001-08-16 Brush seal, assembly of the brush seal, and method of forming the brush seal
DE60106861T DE60106861T2 (en) 2000-09-08 2001-08-16 HEAT-RESISTANT BASE BODY FROM MAGNETIC SILICONE RUBBER FOR A BRUSH SEAL IN TURBOMAS AND METHOD FOR THEIR USE
PCT/US2001/025617 WO2002021027A1 (en) 2000-09-08 2001-08-16 Heat-resistance magnetic silicone rubber body for brush seals in turbomachinery and methods of application

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US09/657,527 US6390476B1 (en) 2000-09-08 2000-09-08 Heat-resistant magnetic silicone rubber brush seals in turbomachinery and methods of application

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EP (1) EP1234130B1 (en)
JP (1) JP2004508520A (en)
AT (1) ATE281618T1 (en)
DE (1) DE60106861T2 (en)
WO (1) WO2002021027A1 (en)

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US6517314B1 (en) * 2001-11-05 2003-02-11 General Electric Company Method and apparatus for eliminating thermal bowing and axial thrust loads of steam turbine rotors
US6571470B1 (en) * 2001-12-06 2003-06-03 General Electric Company Method of retrofitting seals in a gas turbine
US20030193146A1 (en) * 2002-04-10 2003-10-16 Addis Mark E. Brush seal with reduced clearance
US20040100033A1 (en) * 2002-11-27 2004-05-27 Wei Tong Sealing apparatus for electrical generator ventilation system
US20040126226A1 (en) * 2002-12-26 2004-07-01 Addis Mark E. Seal
US20050040602A1 (en) * 2003-08-18 2005-02-24 Mtu Aero Engines Gmbh Brush seal
US20050146095A1 (en) * 2002-03-26 2005-07-07 Siemens Aktiengesellschaft Sealing assembly for a spindle
US20060125190A1 (en) * 2004-12-14 2006-06-15 United Technologies Corporation Clamp lock brush seal assembly
US20070063448A1 (en) * 2005-09-22 2007-03-22 General Electric Company Seals for turbines and turbo machinery
US20080148640A1 (en) * 2006-12-22 2008-06-26 Action Industries, Ltd. Flexible brush seal
US20080284107A1 (en) * 2004-05-04 2008-11-20 Flaherty Andrew L Ceramic Brush Seals
US20090218771A1 (en) * 2008-03-03 2009-09-03 Sparks Glenn D Bristle and plate subassembly fixture and manufacturing method
US20100135607A1 (en) * 2009-09-30 2010-06-03 Peter Rogall Seal arrangement and a brush seal for a wind turbine
US20100327534A1 (en) * 2009-06-26 2010-12-30 General Electric Company Magnetic brush seal system
US20120126483A1 (en) * 2005-04-01 2012-05-24 Peter Francis Crudgington Brush seals
US20140117624A1 (en) * 2012-10-31 2014-05-01 General Electric Company Pressure actuated film riding seals for turbo machinery
CN103883363A (en) * 2014-04-02 2014-06-25 江苏透平密封高科技有限公司 Non-contact type brush-type seal and manufacturing method thereof
US20140301848A1 (en) * 2011-11-17 2014-10-09 Alstom Renovables España, S.L. Sealing assembly
US20140300058A1 (en) * 2012-12-05 2014-10-09 Snecma Sealing of turbine engine enclosures produced by brush seal and labyrinth
US9045994B2 (en) * 2012-10-31 2015-06-02 General Electric Company Film riding aerodynamic seals for rotary machines
US20150300189A1 (en) * 2014-04-16 2015-10-22 Siemens Energy, Inc. Interstage seal assembly for gas turbine engine
US20160032750A1 (en) * 2013-07-11 2016-02-04 United Technologies Corporation Stationary non-rotating brush seals
US20160040600A1 (en) * 2013-03-13 2016-02-11 United Technologies Corporation Multi-axial brush seal
US9718087B1 (en) 2013-03-15 2017-08-01 The Sherwin-Williams Company Treated applicator to increase performance
CN107208801A (en) * 2015-03-09 2017-09-26 伊格尔工业股份有限公司 The assemble method of Splittable brush seal installation, brush seal piece and Splittable brush seal installation
US10161259B2 (en) 2014-10-28 2018-12-25 General Electric Company Flexible film-riding seal

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KR101633546B1 (en) * 2014-06-17 2016-06-24 두산중공업 주식회사 Brush seal assembly
EP3293360A1 (en) * 2016-09-13 2018-03-14 United Technologies Corporation Seal system with primary and secondary seal arrangement
CN108757055B (en) * 2018-05-24 2020-07-28 西安交通大学 A labyrinth sealing structure with brush type sealing strip

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US5090710A (en) 1987-05-29 1992-02-25 Cross Manufacturing Company (1938) Limited Brush seals
US5400586A (en) 1992-07-28 1995-03-28 General Electric Co. Self-accommodating brush seal for gas turbine combustor
US5630590A (en) * 1996-03-26 1997-05-20 United Technologies Corporation Method and apparatus for improving the airsealing effectiveness in a turbine engine
US6027121A (en) * 1997-10-23 2000-02-22 General Electric Co. Combined brush/labyrinth seal for rotary machines
US6257588B1 (en) * 1998-09-22 2001-07-10 General Electric Company Brush seal and rotary machine including such brush seal

Cited By (45)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6517314B1 (en) * 2001-11-05 2003-02-11 General Electric Company Method and apparatus for eliminating thermal bowing and axial thrust loads of steam turbine rotors
US6571470B1 (en) * 2001-12-06 2003-06-03 General Electric Company Method of retrofitting seals in a gas turbine
US20050146095A1 (en) * 2002-03-26 2005-07-07 Siemens Aktiengesellschaft Sealing assembly for a spindle
US7677847B2 (en) * 2002-03-26 2010-03-16 Siemens Aktiengesellschaft Sealing assembly for a spindle
US20030193146A1 (en) * 2002-04-10 2003-10-16 Addis Mark E. Brush seal with reduced clearance
US20040100033A1 (en) * 2002-11-27 2004-05-27 Wei Tong Sealing apparatus for electrical generator ventilation system
US6779799B2 (en) * 2002-11-27 2004-08-24 General Electric Company Sealing apparatus for electrical generator ventilation system
US20040126226A1 (en) * 2002-12-26 2004-07-01 Addis Mark E. Seal
US6910857B2 (en) * 2002-12-26 2005-06-28 United Technologies Corporation Seal
GB2406149B (en) * 2003-08-18 2007-03-28 Mtu Aero Engines Gmbh Brush seal
US20050040602A1 (en) * 2003-08-18 2005-02-24 Mtu Aero Engines Gmbh Brush seal
GB2406149A (en) * 2003-08-18 2005-03-23 Mtu Aero Engines Gmbh A brush seal assembly for a turbine engine
US7644928B2 (en) 2003-08-18 2010-01-12 Mtu Aero Engines Gmbh Brush seal
US20080284107A1 (en) * 2004-05-04 2008-11-20 Flaherty Andrew L Ceramic Brush Seals
US7226054B2 (en) * 2004-12-14 2007-06-05 United Technologies Corporation Clamp lock brush seal assembly
US20060125190A1 (en) * 2004-12-14 2006-06-15 United Technologies Corporation Clamp lock brush seal assembly
US8840113B2 (en) * 2005-04-01 2014-09-23 Cross Manufacturing Company (1938) Limited Brush seals
US20120126483A1 (en) * 2005-04-01 2012-05-24 Peter Francis Crudgington Brush seals
US7604241B2 (en) 2005-09-22 2009-10-20 General Electric Company Seals for turbines and turbo machinery
US20070063448A1 (en) * 2005-09-22 2007-03-22 General Electric Company Seals for turbines and turbo machinery
US20080148640A1 (en) * 2006-12-22 2008-06-26 Action Industries, Ltd. Flexible brush seal
US20090218771A1 (en) * 2008-03-03 2009-09-03 Sparks Glenn D Bristle and plate subassembly fixture and manufacturing method
US8528178B2 (en) * 2008-03-03 2013-09-10 United Technologies Corporation Bristle and plate subassembly fixture and manufacturing method
US20100327534A1 (en) * 2009-06-26 2010-12-30 General Electric Company Magnetic brush seal system
US8043012B2 (en) 2009-09-30 2011-10-25 General Electric Company Seal arrangement and a brush seal for a wind turbine
US20100135607A1 (en) * 2009-09-30 2010-06-03 Peter Rogall Seal arrangement and a brush seal for a wind turbine
US20140301848A1 (en) * 2011-11-17 2014-10-09 Alstom Renovables España, S.L. Sealing assembly
US9759329B2 (en) * 2011-11-17 2017-09-12 Alstom Renewable Technologies Sealing assembly
US20140117624A1 (en) * 2012-10-31 2014-05-01 General Electric Company Pressure actuated film riding seals for turbo machinery
US9045994B2 (en) * 2012-10-31 2015-06-02 General Electric Company Film riding aerodynamic seals for rotary machines
US9115810B2 (en) * 2012-10-31 2015-08-25 General Electric Company Pressure actuated film riding seals for turbo machinery
US9879607B2 (en) * 2012-12-05 2018-01-30 Snecma Sealing of turbine engine enclosures produced by brush seal and labyrinth
US20140300058A1 (en) * 2012-12-05 2014-10-09 Snecma Sealing of turbine engine enclosures produced by brush seal and labyrinth
US20160040600A1 (en) * 2013-03-13 2016-02-11 United Technologies Corporation Multi-axial brush seal
US10208674B2 (en) * 2013-03-13 2019-02-19 United Technologies Corporation Multi-axial brush seal
US9718087B1 (en) 2013-03-15 2017-08-01 The Sherwin-Williams Company Treated applicator to increase performance
US20160032750A1 (en) * 2013-07-11 2016-02-04 United Technologies Corporation Stationary non-rotating brush seals
US9702260B2 (en) * 2013-07-11 2017-07-11 United Technologies Corporation Stationary non-rotating brush seals
CN103883363B (en) * 2014-04-02 2015-10-28 江苏透平密封高科技股份有限公司 A kind of contactless brush seal and preparation method thereof
CN103883363A (en) * 2014-04-02 2014-06-25 江苏透平密封高科技有限公司 Non-contact type brush-type seal and manufacturing method thereof
US9540941B2 (en) * 2014-04-16 2017-01-10 Siemens Energy, Inc. Interstage seal assembly for gas turbine engine
US20150300189A1 (en) * 2014-04-16 2015-10-22 Siemens Energy, Inc. Interstage seal assembly for gas turbine engine
US10161259B2 (en) 2014-10-28 2018-12-25 General Electric Company Flexible film-riding seal
CN107208801A (en) * 2015-03-09 2017-09-26 伊格尔工业股份有限公司 The assemble method of Splittable brush seal installation, brush seal piece and Splittable brush seal installation
US10502322B2 (en) 2015-03-09 2019-12-10 Eagle Industry Co., Ltd. Split type brush seal device, brush seal pieces, and method of assembling split type brush seal device

Also Published As

Publication number Publication date
ATE281618T1 (en) 2004-11-15
EP1234130B1 (en) 2004-11-03
EP1234130A1 (en) 2002-08-28
WO2002021027A8 (en) 2002-06-20
DE60106861T2 (en) 2005-11-10
JP2004508520A (en) 2004-03-18
DE60106861D1 (en) 2004-12-09
WO2002021027A1 (en) 2002-03-14

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